Turbocharger wheel and method of balancing the same

Patent metadata

Field	Value
Publication number	US-2016265359-A1
Application number	US-201514642606-A
Country	US
Kind code	A1
Filing date	Mar 9, 2015
Priority date	Mar 9, 2015
Publication date	Sep 15, 2016
Grant date	—

Abstract

A wheel of a turbocharger includes a first end opposite a second end and a rotational axis extending between the first end and the second end. The wheel also includes a back wall located at the second end and a balance groove formed in the back wall. The balance groove has a plurality of side walls and a bottom surface. The side walls and the bottom surface of the balance groove are milled surfaces.

First claim

What is claimed is:

1 . A wheel of a turbocharger, the wheel comprising:
a first end opposite a second end; a rotational axis extending between the first end and the second end; a back wall located at the second end; and a balance groove formed in the back wall, the balance groove having a plurality of side walls and a bottom surface; wherein the side walls and the bottom surface of the balance groove are milled surfaces.

2 . The wheel of claim 1 , wherein the plurality of side walls include:
first and second side walls that each extend in a radial direction with respect to the rotational axis of the wheel; and third and fourth side walls that each extend in a circumferential direction with respect to the rotational axis of the wheel.

3 . The wheel of claim 2 , wherein:
each of the plurality of side walls curve inward toward the bottom surface of the balance groove; and each of the first, second, third, and fourth side walls has a smooth curvature and connects a surface of the back wall to the bottom surface of the balance groove.

4 . The wheel of claim 2 , wherein the first and second side walls are separated by an angle of about 20° to about 30°.

5 . The wheel of claim 2 , wherein the third and fourth side walls are separated by about 16 mm or less, the third side wall is located a first distance from the rotational axis of the wheel, and the fourth side wall is located a second distance from the rotational axis, the second distance being greater than the first distance.

6 . The wheel of claim 1 , wherein each of the milled surfaces has a surface finish with a cusp height of about 0.02 mm or less.

7 . The wheel of claim 1 , wherein the balance groove has a depth that is less than a radius of curvature of each of the side walls.

8 . The wheel of claim 1 , wherein the balance groove has a depth of about 1 mm or less, the depth being a distance between a surface of the back wall and a surface of the balance groove; and each of the side walls has a radius of curvature of about 5 mm or less.

9 . The wheel of claim 1 , wherein the balance groove is located in an outer ring of the back wall defined by an outer half of a radius of the back wall.

10 . The wheel of claim 1 , wherein:
the wheel is formed integrally as a single-piece component, and is a compressor wheel or a turbine wheel; and the wheel further includes:
a hub extending along the rotational axis of the wheel between a nose located at the first end and the back wall located at the second end; and
a plurality of blades extending from the hub.

11 . A wheel of a turbocharger, the wheel comprising:
a first end opposite a second end; a rotational axis extending between the first end and the second end; a back wall located at the second end; and a balance groove formed in the back wall, the balance groove having a plurality of side walls and a bottom surface, the side walls including:
first and second side walls that each extend in a radial direction with respect to the rotational axis of the wheel, each of the first and second side walls curving inward toward the bottom surface of the balance groove, and
third and fourth side walls that each extend in a circumferential direction with respect to the rotational axis of the wheel, each of the third and fourth side walls curving inward toward the bottom surface of the balance groove;
wherein the wheel is formed integrally as a single-piece component, the side walls and the bottom surface of the balance groove are milled surfaces, and each pair of adjacent side walls intersect to form a curved surface.

12 . The wheel of claim 11 , wherein the intersections of the side walls and the bottom surface are formed without angled corners.

13 . A method of balancing a wheel of a turbocharger, the wheel including a first end opposite a second end and a rotational axis extending between the first end and the second end, the wheel further including a back wall located at the second end, the method comprising:
forming a balance groove in the back wall by removing material from the back wall using a milling tool, forming the balance groove including forming a plurality of side walls of the balance groove using the milling tool.

14 . The method of claim 13 , wherein forming the plurality of side walls using the milling tool includes:
forming first and second side walls of the plurality of side walls using the milling tool, each of the first and second side walls extending in a radial direction with respect to the rotational axis of the wheel, each of the first and second side walls being straight or curving inward toward a bottom surface of the balance groove; and forming third and fourth side walls of the plurality of side walls using the milling tool, each of the third and fourth side walls extending in a circumferential direction with respect to the rotational axis of the wheel, each of the third and fourth side walls being straight or curving inward toward the bottom surface of the balance groove.

15 . The method of claim 13 , further including:
using a milling machine including the milling tool to form the balance groove; and before removing the material to form the balance groove, inputting information for controlling the material removal into the milling machine.

16 . The method of claim 15 , wherein:
the information for controlling the material removal includes at least one of a location or a size of the balance groove; and the milling machine automatically controls at least one of a cutting speed or a feed rate for forming the balance groove based on the information for controlling the material removal.

17 . The method of claim 15 , further including:
before removing the material to form the balance groove, using a balancing machine to perform a balance test on the wheel; and determining the information for controlling the material removal based on the balance test.

18 . The method of claim 17 , further including:
determining at least one unbalance characteristic of the wheel using the balancing machine; and determining the information for controlling the material removal based on the at least one unbalance characteristic using the balancing machine.

19 . The method of claim 18 , wherein the at least one unbalance characteristic includes a magnitude and a direction of an unbalanced force in the wheel.

20 . The method of claim 13 , wherein the milling tool includes a ball end mill.

Assignees

• Caterpillar Inc

Inventors

• Annati Richard E
• Frick Matthew J
• Hogge Douglas G

Classifications

• F04D29/662

  Balancing of rotors (compensating imbalance G01M1/36) · CPC title

• F05D2230/10

  by removing material · CPC title

• F01D5/34

  Rotor-blade aggregates of unitary construction {, e.g. formed of sheet laminae; (discs formed of sheet laminae F01D5/028; ceramic materials F01D5/284, composite materials F01D5/282)} · CPC title

• F02B33/40

  of non-positive-displacement type · CPC title

• F05D2260/15

  Load balancing · CPC title